Guidance, Flight Mechanics and Trajectory Optimization
Author:
Publisher:
Published: 1968
Total Pages: 156
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author:
Publisher:
Published: 1968
Total Pages: 156
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
Published:
Total Pages: 472
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1992
Total Pages: 1572
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
Published: 1969
Total Pages: 470
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. Superintendent of Documents
Publisher:
Published: 1968
Total Pages:
ISBN-13:
DOWNLOAD EBOOKFebruary issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index
Author:
Publisher:
Published: 1970
Total Pages: 232
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1990
Total Pages: 1312
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1972
Total Pages: 1074
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. Superintendent of Documents
Publisher:
Published: 1979
Total Pages: 1504
ISBN-13:
DOWNLOAD EBOOKAuthor: Wanchun Chen
Publisher: Springer Nature
Published: 2020-11-07
Total Pages: 461
ISBN-13: 9811589011
DOWNLOAD EBOOKThis book presents the latest researches on hypersonic steady glide dynamics and guidance, including the concept of steady glide reentry trajectory and the stability of its regular perturbation solutions, trajectory damping control technique for hypersonic glide reentry, singular perturbation guidance of hypersonic glide reentry, trajectory optimization based on steady glide, linear pseudospectral generalized nominal effort miss distance guidance, analytical entry guidance and trajectory-shaping guidance with final speed and load factor constraints. They can be used to solve many new difficult problems in entry guidance. And many practical engineering cases are provided for the readers for better understanding. Researchers and students in the fields of flight vehicle design or flight dynamics, guidance and control could use the book as valuable reference.